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ECIV 720 A Advanced Structural Mechanics and Analysis. Lecture 12: Isoparametric CST Area Coordinates Shape Functions Strain-Displacement Matrix Rayleigh-Ritz Formulation Galerkin Formulation. FEM Solution: Area Triangulation. Area is Discretized into Triangular Shapes.
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ECIV 720 A Advanced Structural Mechanics and Analysis Lecture 12: Isoparametric CST Area Coordinates Shape Functions Strain-Displacement Matrix Rayleigh-Ritz Formulation Galerkin Formulation
FEM Solution: Area Triangulation Area is Discretized into Triangular Shapes
FEM Solution: Area Triangulation One Source of Approximation
FEM Solution: Nodes and Elements Points where corners of triangles meet Define NODES
Non-Acceptable Triangulation … Nodes should be defined on corners of ALL adjacent triangles
FEM Solution: Nodes and Elements vi ui Y X Each node translates in X and Y
FEM Solution: Objective v q6 u q5 3 (x3,y3) q4 q1 q3 q2 2 (x2,y2) 1 (x1,y1) • Use Finite Elements to Compute Approximate Solution At Nodes • Interpolate u and v at any point from Nodal values q1,q2,…q6
Intrinsic Coordinate System 3 (x3,y3) h x 2 (x2,y2) 1 (x1,y1) h x Map Element Define Transformation 2 (0,1) 3 (0,0) 1 (1,0) Parent
Area Coordinates 2 Y A1 P X 3 1 Location of P can be defined uniquely Area Coordinates
Area Coordinates and Shape Functions 3 (x3,y3) x 2 (x2,y2) h 1 (x1,y1) h 2 (0,1) x 3 (0,0) 1 (1,0) Area Coordinates are linear functions of x and h Are equal to 1 at nodes they correspond to Are equal to 0 at all other nodes Natural Choice for Shape Functions
Shape Functions 3 (x3,y3) Y X 2 (x2,y2) x 1 (x1,y1) h
Intrinsic Coordinate System 3 (x3,y3) Map Element Transformation h x 2 (x2,y2) 2 (0,1) 1 (x1,y1) h x 3 (0,0) 1 (1,0) Parent
Displacement Field from Nodal Values 3 q6 v u q5 1 2 x h q4 q2 q3 q1
Strain Tensor from Nodal Values of Displacements Need Derivatives Strain Tensor u and v functions of x and h
Jacobian of Transformation J Jacobian of Transformation J
Jacobian of Transformation – Physical Significance 3 (x3,y3) r1 r2 x 2 (x2,y2) 1 (x1,y1) h
Jacobian of Transformation – Physical Significance k 3 (x3,y3) r1 r2 x 2 (x2,y2) 1 (x1,y1) h Compare to Jacobian
Jacobian of Transformation Solve Solve
Strain Tensor from Nodal Values of Displacements q B e= B q Looks Familiar?
Strain-Displacement Matrix 3 (x3,y3) 2 (x2,y2) x 1 (x1,y1) h Is constant within each element - CST
Stresses e= B q
Element Stiffness Matrix ke 3 (x3,y3) 2 (x2,y2) x 1 (x1,y1) h e= B q s= DB qe ke
Formulation of Stiffness Equations y T (force/area) x z Tt(force/length) y P P x t Assume Plane Stress
Total Potential Approach Tt(force/length) P Total Potential
Total Potential Approach Tt(force/length) P
Total Potential Approach Work Potential of Body Forces
WP of Body Forces 2 Element e fx u fy 3 v 1
WP of Body Forces 3 q6 v u q5 1 2 x h q4 q2 q3 q1
WP of Body Forces 3 q6 v u q5 1 2 x h q4 q2 q3 q1
WP of Body Forces Nodal Equivalent Body Force Vector
Total Potential Approach Work Potential of Tractions
WP of Traction Tt(force/length) 2 3 1 Distributed Load acting on EDGE of element
WP of Traction Components Normal Pressure Tx1,Ty1 p1, p2 Known Distribution Known Distribution Tx2,Ty2
WP of Traction Directional cos Ty2 Tx2 Ty1 Tx1 Normal Pressure p1, p2 Known Distribution Components
WP of Traction 2 v Ty u 3 Tx 1
WP of Traction Ty1 Ty2 Tx1 Tx2 2 3 1
WP of Traction Nodal Equivalent Traction Vector
Total Potential Approach Work Potential of Concentrated Loads
WP of Concentrated Loads P Indicates that at location of point loads a node must be defined
After Superposition Minimizing wrt Q
Galerkin Approach Tt(force/length) P Galerkin
Galerkin Approach Tt(force/length) P
Galerkin Approach 3 y6 fy fx y5 1 2 x h y4 y2 y3 y1 Introduce Virtual Displacement Field f
Galerkin Approach Virtual Strain Energy of element e